Airfoil database search
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
(e379-il) EPPLER 379 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E379 ultralight airfoil Max thickness 2.2% at 5.8% chord Max camber 8% at 31.8% chord Max Cl/Cd 128 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(la203a-il) DOUGLAS LA203A AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Douglas/Liebeck LA203A high lift airfoil Max thickness 15.7% at 34.3% chord Max camber 5.5% at 46% chord Max Cl/Cd 127.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e399-il) EPPLER 399 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E399 human powered aircraft airfoil Max thickness 14.8% at 29% chord Max camber 5.1% at 51.4% chord Max Cl/Cd 127.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(lrn1015-il) NASA LRN 1015 (NASA TM 102840) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | LRN 1015 airfoil used on the Northrop Grumman RQ-4 Global Hawk airfoil Max thickness 15.2% at 40% chord Max camber 4.9% at 44% chord Max Cl/Cd 127.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(ah63k127-il) AH 63-K-127/24 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 63-K-127/24 airfoil for use with flaps (K) Max thickness 12.7% at 40.2% chord Max camber 3.8% at 43.5% chord Max Cl/Cd 127.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(uag8814320-il) UAG 88-143/20 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | UAG 88-143/20 airfoil Max thickness 14.3% at 43.5% chord Max camber 6.2% at 46.7% chord Max Cl/Cd 127 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(psu94097-il) PSU 94-097 (AIAA 2001-2478) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Maughmer PSU 94-097 winglet airfoil Max thickness 9.7% at 32.3% chord Max camber 4% at 46.3% chord Max Cl/Cd 126.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe15-il) GOE 15 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 15 airfoil Max thickness 9% at 29.8% chord Max camber 7.8% at 29.8% chord Max Cl/Cd 126.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(fx67k150-il) FX 67-K-150/17 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 67-K-150/17 airfoil Max thickness 15% at 40.2% chord Max camber 4.8% at 43.5% chord Max Cl/Cd 126.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e657-il) EPPLER 657 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E657 sailplane airfoil Max thickness 15.6% at 37% chord Max camber 4.6% at 47.6% chord Max Cl/Cd 126.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
Please see the source web site or designer for any license conditions.